Parallel algorithm developed on multiple-microprocessor computer. Program initiated to develop computer codes capable of directly simulating and mathematically modeling transition process at mach numbers ranging from subsonic to hypersonic. Parallel computers potentially offer reduction of processing time; processing time inversely proportional to number of available processors.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Computing Flow Transition On Parallel Processors


    Beteiligte:
    Bokhari, S. (Autor:in) / Erlebacher, G. (Autor:in) / Hussaini, M. Y. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.10.1993



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Airfoil design utilizing parallel processors

    Brawley, Stephen C. / Hobson, Garth V. | AIAA | 1996



    Fast, Massively Parallel Data Processors

    Heaton, Robert A. / Blevins, Donald W. / Davis, ED | NTRS | 1994


    Airfoil Design Utilizing Parallel Processors

    Brawley, S.C. | Online Contents | 1996


    Turbine blade design using parallel processors

    Brawley, Stephen / Hobson, Garth | AIAA | 1996